ATLAS 5 CENTAUR DEB, 43958
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 43958 is space debris in HEO originally from a launch on Wed, 17 Sep 2014 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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43958 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 1 week ago
0 ATLAS 5 CENTAUR DEB
1 43958U 14055M 25193.32157232 -.00000021 00000-0 00000+0 0 9992
2 43958 19.8445 168.8198 4774131 121.6823 293.6961 1.89316005 47452
Epoch: 2025-07-12T07:43Z
TLE epoch observation values (Epoch: 2025-07-12T07:43:03.848Z)
Latitude
-0.00003°
Longitude
122.53265°
Altitude
22,058.439 km
Speed
3.687 km/s
True Right ascension
11h 15m 02s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
-18.20099°
Longitude
56.35637°
Altitude
33,893.982 km
Speed
2.314 km/s
Apparent Right ascension
06h 20m 55s
Apparent Declination
-23° 35' 26"
Sunlit
Visualization observer readout
Local Sidereal Time
12:28:06
Azimuth
252.518° W
Elevation
-16.192°
Doppler factor
1
Orbital elements
Apogee altitude
34,404.607 km
Perigee altitude
8,047.434 km
Semi-major axis
27,604.157 km
Eccentricity
0.47741
Inclination
19.8445°
RAAN
168.8198°
Arg. of periapsis
121.6823°
True anomaly
238.36363°
Mean anomaly
293.6961°
Eccentric anomaly
266.39643°
Mean motion
0.47324 °/min
Orbital period
760.71 mins
BSTAR
0
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Other satellites on launch #55 in the year 2014 (2014-09-17 UTC)
ATLAS 5 CENTAUR DEB Visibility forecast
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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101 mins | 2025-07-19 05:55:28.144Z | 264.994° W | 2025-07-19 06:48:28.144Z | 195.058° SSW | 37.658° | 2025-07-19 07:36:28.144Z | 123.458° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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